Attachment for thermal probe

Abstract: A twist-lock (36) for attaching a plastics shell (16) of a thermal probe (18) to a structural member such as a plastics intake manifold (10) of an internal combustion engine in a socket (14) in the structural member. The twist-lock includes hooks (50) on the plastics shell (16) which traverse an annular shoulder (38) at the bottom of the socket (14) through notches (46) in the shoulder (38) when the shell (16) is inserted in the socket (14) and which are captured by the shoulder (38) when the shell (16) is rotated in the socket (14) from an unlocked position to a locked position. The twist-lock (36) further includes a lug (68) on the shell (16) which co-operates with a cam edge (70) on a resilient lip (60) around an open end of the socket (14) to afford tactile representation of the progress of the shell (16) towards, and achievement of, the locked position and to prevent reverse rotation of the shell (16) from the locked position.

Description: This invention relates to a connection assembly for attaching a plastics shell of a thermal probe to a plastics structural member as specified in the preamble of claim 1, and disclosed in DE-A-1 802 520. US Patent No 5046857, issued 10 September 1991, describes a thermal probe assembly having a pre-moulded unitary one-piece plastics shell which attaches to a structural member, e.g. a plastics intake manifold of an internal combustion engine, through male screw threads on the shell and female screw threads in a socket on the manifold. Manufacturing costs associated with fabricating male and female plastics screw threads are relatively high. A twist-lock according to this invention for attaching a plastics shell of a thermal probe to a plastics structural member such as an internal combustion engine intake manifold is an improvement relative to the thermal probe attachment described in the aforesaid US Patent No 5046857. A connection assembly according to the present invention is characterised over DE-A-1 802 520 by the features specified in the characterising portion of claim 1. This invention is a new and improved twist-lock for attaching a plastics shell of a thermal probe to a plastics structural member such as an internal combustion engine intake manifold. The twist-lock according to this invention includes axial retention features on a cylindrical socket in the structural member and on the shell which co-operate when the shell is rotated in the socket from an unlocked position to a locked position to prevent dislodgement of the shell from the socket, and circumferential retention features on the socket and on the shell which co-operate to prevent reverse rotation of the shell from the locked position. The axial retention features include an annular shoulder at the bottom of the socket and a plurality of hooks on the shell which traverse the plane of the shoulder through notches therein when the shell is inserted in the socket and which are captured by the shoulder when the shell is rotated to the locked position. The circumferential retention features include a pair of radial lugs on the plastics shell and an annular lip around an open end of the socket having cam edges therein. When the shell is manually rotated toward the locked position, force reactions between the lugs and ramps of the cam edges effect progressively increasing resilient deflection of the lip and correspondingly increasing resistance to rotation of the shell so that an installer experiences tactile indication of the progress of the installation. The ramps are contiguous with seats of the cam edges which capture the lugs in the locked position of the shell. Sharp discontinuities of the cam edges between the ramps and seats afford tactile and audible indication of achievement of the locked position. The invention and how it may be performed are hereinafter particularly described with reference to the accompanying drawings, in which: Figure 1 is a partially broken-away elevational view of a thermal probe including a plastics shell having a twist-lock according to this invention and showing the thermal probe prior to installation on a plastics structural member; Figure 2 is a sectional view taken generally along the plane indicated by lines 2-2 in Figure 1; Figure 3 is a sectional view taken generally along the plane indicated by lines 3-3 in Figure 1; Figure 4 is a sectional view taken generally along the plane indicated by lines 4-4 in Figure 1; and Figure 5 is similar to Figure 1 but showing the thermal probe after installation on the structural member. Referring to Figures 1-3, a fragmentarily illustrated plastics structural member in the form of a plastics intake manifold 10 of an internal combustion engine, not shown, includes an internal chamber forming an induction passage 12 and a cylindrical socket 14. A one-piece, moulded plastics shell 16 of a thermal probe 18 for monitoring the temperature of air in the induction passage 12 is disposed in the socket 14. A thermistor 20 of the probe is supported below a tubular portion 22 of the shell 16 by a pair of elongated metal terminals 24 each having a pin end 26 in a receptacle portion 28 of the shell. A plastics pre-mould 30 around the terminals is pressed into an appropriately configured passage 32 in the shell with a gas-sealing elastomeric ring 34 therebetween whereby the terminals and the thermistor are attached to the shell. For a more complete description of the thermal probe 18, reference may be made to the aforesaid US patent No 5046857. The shell 16 is attached to the manifold 10 by a twist-lock 36 according to this invention. The twist-lock 36 has axial retention features for preventing dislodgement of the shell 16 from the socket 14 including an annular shoulder 38 at the bottom of the socket 14, an annular flange 40 around the shell 16 between the tubular portion 22 and the receptacle portion 28, and a cage 42 at the distal end of the tubular portion 22. The annular shoulder 38 has an inside perimeter 44 corresponding generally to the perimeter of the tubular portion 22 and is pierced by an asymmetric array of notches 46 each open through the inside perimeter 44. The cage 42 surrounds the thermistor 20 and includes a plurality of radial legs 48 integral with the tubular portion 22 and defining an asymmetric array therearound, see Figure 3, corresponding in size and angular interval to the asymmetric array of notches 46 in the shoulder 38. Each of the legs 48 terminates at a flat hook 50 in a common plane perpendicular to a centreline 52 of the shell Figure 1. The flat hooks 50 are separated from an annular surface 54 of the flange 40 in a plane perpendicular to the centreline 52 by a length dimension L1 of the shell, see Figure 1. The length dimension L1 of the shell corresponds to a length dimension L2, see Figure 1, of the socket 14 between an annular surface 56 of the shoulder 38 and an annular surface 58 defining the top of a reduced section annular lip 60 at the open end of the socket 14. The shell 16 is inserted into the socket 14 with the tubular portion 22 first and has an unlocked position in the socket characterised by seating engagement of the surface 54 of the flange 40 against the surface 58 of the lip 60 and coincidence between the centreline 52 of the shell and a centreline 62 of the socket. Relative to the socket 14, the unlocked position of the shell 16 is unique because the legs 48 can only traverse the plane of the shoulder 38 through the notches 46 when the asymmetric arrays of legs 48 and notches 46 are in angular registry with one another. In the unlocked position of the shell, the hooks 50 on the legs 48 are closely adjacent but slightly below the plane of the annular surface 56 of the shoulder 38. An elastomeric seal ring 64 in a groove in the shell 16 seats against the cylindrical wall of the socket 14 to define a gas-tight seal between the shell and the socket. The shell 16 has a locked position, see Figure 5, achieved by rotating, i.e., twisting, the shell 16 relative to the socket 14 about the coincident centrelines 52,62 through an included angle of 60 degrees from the unlocked position. A pair of finger tabs 66, see Figures 1-3, on the shell 16 afford a convenient manual grip for twisting the shell 16 from the unlocked to the locked position. In the locked position of the shell 16, the asymmetric arrays of legs 48 and notches 46 are out of angular registry with one another so that the surface 56 on the shoulder 38 captures the hooks 50 on the legs 48 to prevent dislodgement of the shell 16 from the socket 14. The twist-lock 36 also has circumferential retention features for preventing reverse rotation of the shell 16 from the locked position thereof including a pair of radial lugs 68 integral with and located on opposite sides of the shell adjacent the annular flange 40 and a pair of cam edges 70 located diametrically opposite each other on an inside cylindrical wall 72 of the lip 60, Figure 4. The cam edges 70 each include a ramp 74 and a seat 76 contiguous with the ramp. Each ramp has an outboard end radially outwards of the inside cylindrical wall 72 and an inboard end closer to the inside cylindrical wall. The junction of the inboard end of each ramp and the corresponding seat 76 is characterised by a sharp discontinuity in the form of a step 78, see Figure 4. The radial depth of the seats 76 corresponds generally to the radial depth of the outboard ends of the ramps. The cam edges 70 are located relative to the notches 46 and the legs 48 such that, in the aforesaid unlocked position of the shell 16, the lugs 68 are disposed at respective ones of the outboard ends of the ramps, and in the aforesaid locked position, the lugs 68 are disposed in respective ones of the seats 76. When the shell is rotated about the coincident centrelines 52,62 from the unlocked position toward the locked position by application of manual effort at the finger tabs 66, the lugs 68 engage the ramps 74. The force reactions between the lugs and the ramps include radial forces on the inside cylindrical wall 72 effecting resilient outward deflection of the lip 60 and tangential forces on the lugs 68 resisting rotation of the shell 16 towards the locked position. The radial and tangential force reactions increase as the lugs 68 approach the seats 76 due to the increasing interference between the ramps 74 and the lugs 68 and afford an installer tactile indication of the progress of the installation of the thermal probe. At the instant the lugs traverse the steps 78 between the ramps 74 and the seats 76, the aforesaid radial and tangential force reactions are relieved and afforded both tactile and audible indications of achievement of the locked position. In addition, the steps 78 block movement of the lugs 68 in the opposite direction to prevent reverse rotation of the shell from the locked position towards the unlocked position except upon application of a high level of manual effort at the finger tabs 66 indicative of or corresponding to a conscious intent to remove the thermal probe 18 from the socket 14.

Claims: A connection assembly between a structural member (10) and the thermal probe (18), the structural member (10) having a fluid medium chamber (12) and a cylindrical socket (14), and the thermal probe (18) having a plastics shell (16) adapted for disposition in said socket (14) to monitor the temperature of a fluid medium in said fluid medium chamber (12), characterised in that the connection assembly is a twist-lock (36) comprising: an annular shoulder (38) on said socket (14), the shoulder having an inside perimeter (44) and a circumferential array of a plurality of notches (46) open through said inside perimeter (44); a plurality of radial legs (48) on said shell (16) each having thereon a hook (50) and being arranged in an angular array around said shell (16) corresponding to said circumferential array of notches (46) in said annular shoulder (38) so that an unlocked position of said shell (16) relative to said socket (14) is defined by angular registry between said circumferential array of notches (46) and said angular array of radial legs (48); means (54,58) on said socket (14) and on said shell (16) operative to limit penetration of said shell (16) into said socket (14) such that, in said unlocked position of said shell (16), said hooks (50) are disposed in said fluid medium chamber (12) closely adjacent the plane of a planar surface (56) of said annular shoulder (38) so that, when said shell (16) is manually rotated in said socket (14) from said unlocked position to a locked position, said planar surface (56) captures said hooks (50) and prevents dislodgement of said shell (16) from said socket (14); and cam and lug means (68,70) on said shell (16) and on said socket (14) affording tactile representation of the progress of movement of said shell (16) towards said locked position and of achievement of said locked position during manual rotation of said shell (16) from said unlocked to said locked position and retaining said shell (16) in said locked position. A connection assembly according to claim 1, in which said cam and lug means includes: a lug (68) on one of said shell (16) and said socket (14), and a cam edge (70) on the other of said shell (16) and said socket (14) including a ramp (74) engageable on said lug (68) during rotation of said shell (16) from said unlocked to said locked position and increasingly resisting rotation of said shell (16) towards said locked position, and a seat (76) contiguous with said ramp (74), which confines said lug (68) in said locked position of said shell (16) and prevents reverse rotation of said shell (16) from said locked position towards said unlocked position. A connection assembly according to claim 2, in which said seat (76) defines a sharp discontinuity (78) in said cam edge (70) effecting tactile representation of achievement of said locked position of said shell (16) when said lug (68) traverses said sharp discontinuity (78). A connection assembly according to claim 3, in which said cam and lug means includes: a radially resilient lip (60) around an open end of said socket (14) including an inside cylindrical wall (72), and said cam edge (70) is defined on said inside cylindrical wall (72). A connection assembly according to claim 4, in which said circumferential array of notches (46) in said annular shoulder (38) is asymmetric, and said angular array of radial legs (48) on said shell (16) is correspondingly asymmetric so that said unlocked position of said shell (16) relative to said socket (14) is unique.

Inventors: GEIGER SCOTT ALAN, HESTON JEFFREY WILLIAM, POLANKA MARC DAMIAN, ROCK JEFFREY ALLAN, GEIGER, SCOTT ALAN, HESTON, JEFFREY WILLIAM, POLANKA, MARC DAMIAN, ROCK, JEFFREY ALLAN
Applicants: GEN MOTORS CORP, GENERAL MOTORS CORPORATION
Application year: 1994
Main classification: G01K13
IPC codes: G01K7, F02B77, G01K13, G01K1, F02D35, F02M35